NOZZLE ASSEMBLY
    1.
    发明申请
    NOZZLE ASSEMBLY 有权
    喷嘴组件

    公开(公告)号:US20130255264A1

    公开(公告)日:2013-10-03

    申请号:US12503913

    申请日:2009-07-16

    IPC分类号: F02M61/16

    摘要: A nozzle assembly (10) comprises a first-fuel-inlet tube (80), a second-fuel-inlet tube (90), and a plate stack (100). The nozzle-plate stack (100) defines a central circuit (104), corner air circuits (105), a first fuel circuit (106) and a second fuel circuit (107). The fuel circuits (106, 107) include a swirl chamber in which the fuel is swirled prior to being merged with the central circuit (104). The corner air circuits (105) merge with the central circuit (104) downstream of the fuel circuits' merge and provide an additional swirling component to further shape the fuel-air stream prior to ignition.

    摘要翻译: 喷嘴组件(10)包括第一燃料入口管(80),第二燃料入口管(90)和板堆(100)。 喷嘴板堆叠(100)限定中心电路(104),角空气回路(105),第一燃料回路(106)和第二燃料回路(107)。 燃料回路(106,107)包括涡流室,其中燃料在与中心回路(104)合并之前旋转。 角空气回路(105)与燃料回路下游的中心回路(104)合并,并提供额外的旋流部件,以在点燃之前进一步调节燃料 - 空气流的形状。

    Nozzle assembly
    2.
    发明授权
    Nozzle assembly 有权
    喷嘴总成

    公开(公告)号:US08616003B2

    公开(公告)日:2013-12-31

    申请号:US12503913

    申请日:2009-07-16

    IPC分类号: F02C1/00

    摘要: A nozzle assembly comprises a first-fuel-inlet tube, a second-fuel-inlet tube, and a plate stack. The nozzle-plate stack (100) defines a central circuit, corner air circuits, a first fuel circuit and a second fuel circuit. The fuel circuits include a swirl chamber in which the fuel is swirled prior to being merged with the central circuit. The corner air circuits merge with the central circuit downstream of the fuel circuits' merge and provide an additional swirling component to further shape the fuel-air stream prior to ignition.

    摘要翻译: 喷嘴组件包括第一燃料入口管,第二燃料入口管和板堆。 喷嘴板堆叠(100)限定中央电路,角空气回路,第一燃料电路和第二燃料电路。 燃料回路包括涡流室,其中燃料在与中心回路合并之前旋转。 拐角空气回路与燃料回路下游的中心回路合并,并提供额外的旋流部件,以在点燃之前进一步调整燃料 - 空气流的形状。

    Macrolaminate radial injector
    4.
    发明授权
    Macrolaminate radial injector 有权
    高碘酸钠径向注射器

    公开(公告)号:US07028483B2

    公开(公告)日:2006-04-18

    申请号:US10889842

    申请日:2004-07-13

    IPC分类号: F23R3/28

    摘要: An injector assembly includes a barrel-shaped housing and an injector, the injector including a feed ring formed of multiple, etched, T-shaped plates. A plurality of nozzles are arranged in an evenly-spaced array around the injector and direct fluid radially inward into the central annulus of the injector assembly. The injector includes an air inlet port with an internal feed passage fluidly connected to swirl chambers and exit orifices to provide individual sprays of fuel from the nozzles. Integral air swirlers impart a swirling component of motion to the fuel sprays. A venturi configuration is provided by the housing. The nozzles are provided along the venturi configuration, which maintains fluid separation from the walls of the housing downstream from the venturi.

    摘要翻译: 注射器组件包括筒形壳体和注射器,注射器包括由多个蚀刻的T形板形成的进料环。 多个喷嘴围绕喷射器以均匀间隔的阵列布置,并且将流体径向向内引导到喷射器组件的中心环中。 喷射器包括具有内部进料通道的空气入口,流体连接到涡流室和出口,以从喷嘴提供燃料的单独喷射。 一体式空气旋流器将燃料喷雾的旋转分量赋予运动。 文丘里配置由壳体提供。 沿着文氏管结构设置喷嘴,其保持与文丘里管下游的壳体的壁分离。

    Pure airblast nozzle
    5.
    发明授权

    公开(公告)号:US06622488B2

    公开(公告)日:2003-09-23

    申请号:US10010216

    申请日:2001-12-07

    IPC分类号: F02C100

    摘要: A fuel injector for a gas turbine engine of an aircraft has an inlet fitting, a fuel nozzle, and a housing stem with an internal conduit fluidly interconnecting the nozzle and fitting. The fuel nozzle includes a fuel swirler, which includes a plenum for receiving fuel from the conduit. A plurality of fuel passages direct fuel from the plenum to discharge orifices. The downstream ends of the passages are angled such that a swirl component is imparted to fuel exiting the discharge orifices. The swirling fuel is then applied to a prefilmer, which outwardly surrounds the fuel swirler. The passages in the fuel swirler are arranged such that the discharge orifices surround the entire nozzle for the even distribution of fuel. The plenum and passages are dimensioned and configured to receive and distribute the fuel for uniform spray patternization and low pressure drop, which provides improved combustion and flame stability.

    Stable pre-mixer for lean burn composition
    6.
    发明授权
    Stable pre-mixer for lean burn composition 有权
    稳定的预混合器用于稀薄燃烧组合物

    公开(公告)号:US06311473B1

    公开(公告)日:2001-11-06

    申请号:US09517823

    申请日:2000-03-02

    IPC分类号: F02C100

    摘要: A combustion system includes a combustion chamber and a fuel injection apparatus, where a radial inflow swirler stage in the injector housing includes a plurality of radial inflow swirlers spaced longitudinally from each other to direct air radially inward in a swirling motion to cause fuel streams to swirl and thoroughly mix with air before passing into the combustion chamber. A plurality of liquid fuel nozzles are supported in the housing in an annular arrangement to dispense liquid fuel in a plurality of sprays in the downstream direction. A plurality of gaseous fuel nozzles are also provided in the housing supported in an annular arrangement intermediate the liquid fuel nozzles. The plurality of gaseous fuel nozzles include a series of nozzles arranged in radial spokes between each of the liquid fuel nozzles, with the size of the openings in the gaseous fuel nozzles increasing in the radially outer direction from the longitudinal axis of the housing. An outer annular flow passage is provided around the nozzles to create a cylindrical sheet of air around all the fuel streams, while an annular flow passage is provided around each of the liquid fuel nozzles to provide an annular flow of air around each of the liquid fuel sprays. A central air passage provides air centrally of the arrangement of nozzles. The air vaporizes the liquid fuel as the fuel passes downstream through the housing.

    摘要翻译: 燃烧系统包括燃烧室和燃料喷射装置,其中喷射器壳体中的径向流入旋流器台包括彼此纵向间隔开的多个径向流入旋流器,以在旋转运动中径向向内引导空气,以使燃料流旋转 并在进入燃烧室之前与空气充分混合。 多个液体燃料喷嘴以环形装置支撑在壳体中,以在下游方向上分配多个喷雾中的液体燃料。 多个气体燃料喷嘴还设置在壳体中,以液体燃料喷嘴中间的环形装置支撑。 多个气体燃料喷嘴包括在每个液体燃料喷嘴之间以径向辐条布置的一系列喷嘴,气态燃料喷嘴中的开口的尺寸在从壳体的纵向轴线的径向外侧方向上增加。 在喷嘴周围设置外部环形流动通道,以围绕所有燃料流形成圆柱形空气,同时在每个液体燃料喷嘴周围设置环形流动通道,以提供围绕每个液体燃料的环形空气流 喷雾 中央空气通道在喷嘴布置的中央提供空气。 当燃料通过壳体的下游时,空气使液体燃料蒸发。

    Low-power force sensor
    7.
    发明授权
    Low-power force sensor 有权
    低功率力传感器

    公开(公告)号:US08534143B2

    公开(公告)日:2013-09-17

    申请号:US12833385

    申请日:2010-07-09

    IPC分类号: G01L1/04 G01L1/00 G01F1/28

    摘要: A force sensor utilizing force sensing element to generate an output signal that is commensurate with the force applied to the sensor. The force sensor includes a support element coupled to a resilient deflectable portion and at least one pivotable arm portion extending from the resilient deflectable portion; and a force sensing element supported by the base element and operably coupled to the at least one pivotable arm portion, wherein the force sensing element outputs an output signal that is proportional to a force applied to the at least one pivotable arm portion. The force sensor may be used a mass flow meter by coupling a fluid passage to the force sensor. The structure of the force sensor makes use of mechanical amplification to greatly increase the sensitivity of the sensor.

    摘要翻译: 利用力传感元件产生与施加到传感器的力相当的输出信号的力传感器。 力传感器包括联接到弹性可偏转部分的支撑元件和从弹性偏转部分延伸的至少一个可枢转臂部分; 以及由所述基座元件支撑并且可操作地联接到所述至少一个可枢转臂部分的力感测元件,其中所述力感测元件输出与施加到所述至少一个可枢转臂部分的力成比例的输出信号。 力传感器可以通过将流体通道联接到力传感器而用于质量流量计。 力传感器的结构利用机械放大,大大增加了传感器的灵敏度。

    Integrated fluid injection air mixing system
    8.
    发明授权
    Integrated fluid injection air mixing system 有权
    集成流体注射空气混合系统

    公开(公告)号:US06533954B2

    公开(公告)日:2003-03-18

    申请号:US09794470

    申请日:2001-02-27

    IPC分类号: B44C122

    CPC分类号: F23D11/103 F23D11/46 F23R3/28

    摘要: An atomizing injector includes a metering set having a swirl chamber, a spray orifice and one or more feed slots etched in a thin plate. The swirl chamber is etched in a first side of the plate and the spray orifice is etched through a second side to the center of the swirl chamber. Fuel feed slots extend non-radially to the swirl chamber. The injector also includes integral swirler structure. The swirler structure includes a cylindrical air swirler passage, also shaped by etching, through at least one other thin plate. The cylindrical air swirler passage is located in co-axial relation to the spray orifice of the plate of the fuel metering set such that fuel directed through the spray orifice passes through the air swirler passage and swirling air is imparted to the fuel such that the fuel has a swirling component of motion. At least one air feed slot is provided in fluid communication with the air swirler passage and extends in non-radial relation thereto. Air supply passages extend through the plates of the metering set and the swirler structure to feed the air feed slot in each plate of the swirler structure.

    摘要翻译: 雾化喷射器包括具有涡流室,喷射孔和蚀刻在薄板中的一个或多个进料槽的计量组。 涡流室在板的第一侧被蚀刻,并且喷嘴通过第二侧蚀刻到涡流室的中心。 燃料供给槽非径向地延伸到涡流室。 注射器还包括整体旋流器结构。 旋流器结构包括通过蚀刻成形的圆柱形空气旋流器通道,通过至少一个其它薄板。 圆柱形空气旋流器通道与燃料计量装置的板的喷孔同轴地定位,使得引导通过喷射孔的燃料通过空气旋流器通道并且旋转空气被赋予燃料,使得燃料 具有运动的旋转分量。 提供至少一个空气供给槽与空气旋流器通道流体连通并以非径向关系延伸。 供气通道延伸穿过计量组和旋流器结构的板,以将旋流器结构的每个板中的供气槽供给。

    Macrolaminate direct injection nozzle
    9.
    发明授权
    Macrolaminate direct injection nozzle 有权
    马来酰胺直喷喷嘴

    公开(公告)号:US07021562B2

    公开(公告)日:2006-04-04

    申请号:US10685691

    申请日:2003-10-14

    摘要: A fuel injector for a gas turbine engine includes a bulkhead having adjacent angled wall segments, each of which includes an injector opening. Fuel injectors are supported by the bulkhead on adjacent wall segments. Each fuel injector includes an inlet fitting including ports for receiving fuel, a feed stem extending through the opening, and a manifold supported at the downstream end of the feed stem and including a plurality of manifold segments. Each manifold segment includes a plurality of nozzles arranged in a linear, planar array; with each nozzle including a fuel distribution assembly and an air swirler assembly. The manifold segments are supported at angles to one another, such that that the sprays from one array of nozzles in one segment are provided in a different direction than the sprays from another array of nozzles in an adjacent manifold segment.

    摘要翻译: 用于燃气涡轮发动机的燃料喷射器包括具有相邻的倾斜壁段的隔板,每个隔板包括喷射器开口。 燃油喷射器由相邻壁段上的舱壁支撑。 每个燃料喷射器包括入口配件,其包括用于接收燃料的端口,延伸穿过开口的进料杆和在进料杆的下游端处支撑并包括多个歧管段的歧管。 每个歧管段包括布置成线性平面阵列的多个喷嘴; 每个喷嘴包括燃料分配组件和空气旋流器组件。 歧管段以彼此成角度的方式被支撑,使得来自一个区段中的一个喷嘴阵列的喷雾以与来自相邻歧管段中的另一喷嘴阵列的喷雾不同的方向设置。

    Multi-function simplex/prefilmer nozzle
    10.
    发明授权
    Multi-function simplex/prefilmer nozzle 有权
    多功能单面/预浸嘴

    公开(公告)号:US06920749B2

    公开(公告)日:2005-07-26

    申请号:US10387001

    申请日:2003-03-11

    摘要: A multi-function spray nozzle for engine applications useful as a cooling device to introduce a fluid into the fluid stream of the engine, and as a cleaning device to introduce a fluid to clean internal components of the engine. The nozzle includes a multi-layered arrangement of etched plates defining flow paths for the first and second fluids. Non-radial feed slots direct the first fluid into a cylindrical swirl chamber. The swirling fluid exits the swirl chamber through a spray orifice or a prefilmer, depending on whether the nozzle is configured as a simplex or prefilmer nozzle. Other non-radial feed slots direct the second fluid inward, downstream of the first fluid, to create a fine dispersion of droplets for fluid stream cooling purposes. During cleaning, only the first fluid is introduced through the nozzle, which results in a larger droplet size suitable for cleaning purposes of the internal components of the engine.

    摘要翻译: 一种用于发动机应用的多功能喷嘴,其用作将流体引入发动机的流体流中的冷却装置,以及用于引入流体以清洁发动机的内部部件的清洁装置。 喷嘴包括限定第一和第二流体的流动路径的蚀刻板的多层布置。 非径向进料槽将第一流体引导到圆柱形旋流室中。 旋转流体通过喷射孔或预吹器离开涡流室,这取决于喷嘴是否被配置为单纯度或预吹扫喷嘴。 其他非径向进料槽将第二流体向内引导到第一流体的下游,以产生用于流体流冷却目的的液滴的精细分散体。 在清洁期间,只有第一流体通过喷嘴引入,这导致适于清洁发动机内部部件的液滴大小。